首页> 外文学位 >A numerical investigation of the unsteady flow and heat transfer in a forced and unforced confined laminar impinging.
【24h】

A numerical investigation of the unsteady flow and heat transfer in a forced and unforced confined laminar impinging.

机译:强迫和非强迫密闭层流撞击中非稳态流动和传热的数值研究。

获取原文
获取原文并翻译 | 示例

摘要

A numerical finite-difference model, derived using a control-volume approach, is used to compute the flow and heat transfer characteristics of a confined laminar air jet impinging on an isothermal surface. Four cases are considered, with Re = 250, 500, 650 and 750, and nozzle-to-plate spacing, H/W = 5.; At Re = 250, the boundary layer developing on the target plate separates. At Re = 500, the boundary layer develops without separation off the target wall, the jet momentum is sufficient to overcome the adverse outer field and wall effects. The flow is symmetric at these Reynolds numbers, and maximum values for pressure, friction and heat transfer coefficients occur at the stagnation point.; The flow at Re = 650 displays asymmetry as the jet buckles, both flow and heat transfer indicate a transition to an unsteady regime. The critical Reynolds number for the onset of unsteady flow is between 585 and 610. When Re is further increased to 750, the jet “buckles” severely and vortices are shed in the high shear regions. The spectral distribution of the velocity in the jet streamwise and spanwise directions at three distinct locations in the jet, point out three dominant frequencies.; The lowest frequency, at 3.66 Hz, is associated with the jet “sweeping” the wall, identified as the “flapping” motion. The highest frequency, 12.96 Hz, is related to the “buckling” motion of the jet at the frequency at which vortices are formed in the jet shear layer. As a result of the two combined unsteady modes, the peak heat transfer is enhanced and the lateral extent of the effective cooling is broadened. A distinct demarcation in time averaged Nusselt number was observed between the steady behavior for Re 600, and the unsteady behavior for Re > 600.; The jet subjected to twenty-four types of forcing reveals two cases relevant in terms of flow and heat transfer control. The out-of-phase forcing at the dominant frequency of 10.68 Hz, Re = 650, stabilizes one side of the confined impinging jet. This results in an enhanced wall heat transfer and peculiar behavior of the hydrodynamic field.; When forcing out-of-phase at a dominant frequency of 12.96 Hz, Re = 75 0, the jet is stabilized completely. The forcing suppresses the high-amplitude low-frequency “flapping” jet motion, and the jet tip displacement on the target wall captures only the high-frequency low-amplitude oscillatory motion of the jet. The suppression of the jet “flapping” motion leads to a smaller “patch” heat transfer coefficient. However, since the jet washes the target wall without separation, the wall-averaged heat transfer is much higher than the unforced cases. For the out-of-phase forcing at 12.96 Hz, the “patch” heat transfer is 24% lower than the unforced case, while the wall-averaged heat transfer is 35% higher.
机译:使用控制体积方法导出的数值有限差分模型用于计算撞击在等温面上的受限层流空气射流的流动和传热特性。考虑了四种情况,Re = 250、500、650和750,喷嘴到板的间距H / W = 5;在Re = 250时,在靶板上形成的边界层分离。在Re = 500时,边界层没有从目标壁分离而形成,射流动量足以克服不利的外场和壁效应。在这些雷诺数下,流动是对称的,压力,摩擦和传热系数的最大值出现在停滞点。 Re = 650时的流量显示出不对称性,因为射流发生弯曲,流量和热传递都表明向不稳定状态过渡。对于不稳定流动的起始雷诺数在585和610之间。当Re进一步增加到750时,射流会严重“扭曲”,并且在高剪切区域会产生涡旋。射流中三个不同位置的射流沿流向和翼展方向的频谱分布指出了三个主频。最低频率为3.66 Hz,与喷射流“扫过”墙壁有关,被称为“拍打”运动。最高频率12.96 Hz与在射流剪切层中形成涡旋的频率下射流的“屈曲”运动有关。由于这两种组合的非稳态模式,峰值传热得到增强,有效冷却的横向范围扩大了。在Re <600的稳定行为与Re> 600的不稳定行为之间,观察到时间平均Nusselt数的明显划分。受到二十四种强迫作用的射流揭示了两种与流量和传热控制有关的情况。主频率为10.68 Hz(Re = 650)时的异相强迫使受限制射流的一侧稳定。这导致增强的壁传热和流体动力场的特殊行为。当以12.96 Hz的主导频率(Re = 75 0)强制异​​相时,射流将完全稳定。强制抑制了高振幅的低频“拍打”喷射运动,并且目标壁上的喷嘴尖端位移仅捕获了射流的高频低振幅振荡运动。射流“拍打”运动的抑制导致较小的“斑片”传热系数。但是,由于射流会冲洗目标壁而不会分离,因此与平均情况相比,壁面平均传热要高得多。对于12.96 Hz的异相强迫,“贴片”传热比非受力情况低24%,而壁平均传热高35%。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号